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公开(公告)号：US20210206505A1
公开(公告)日：2021-07-08
申请号：US17188809
申请日：2021-03-01
Applicant: Safran Nacelles
Inventor： Hakim MAALIOUNE , Julien CORBIN , Alain NOURRISSON , Julien CALMELS , Maxime POUYET
Abstract: An electrical control system intended for an aircraft turbojet engine nacelle includes two control modules of a single power module controlling an electric machine and an approval module linking each of the control modules to the single power module. The approval module selectively authorizes the control of the single power module by one of the control modules.
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